درباره ما
NACA-TM-948
A simple approximation method for obtaining the spanwise lift distribution
Year: 1940
Abstract: The approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method and includes also the important case of the wing with end plates.
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:33:58Z | |
| date available | 2017-09-04T17:33:58Z | |
| date copyright | 01/01/1940 | |
| date issued | 1940 | |
| identifier other | DDYIYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/156789 | |
| description abstract | The approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method and includes also the important case of the wing with end plates. | |
| language | English | |
| title | NACA-TM-948 | num |
| title | A simple approximation method for obtaining the spanwise lift distribution | en |
| type | standard | |
| page | 16 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1940 | |
| contenttype | fulltext |